US20120171502A1 - Process for surface treating magnesium alloy and article made with same - Google Patents

Process for surface treating magnesium alloy and article made with same Download PDF

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US20120171502A1
US20120171502A1 US13/188,575 US201113188575A US2012171502A1 US 20120171502 A1 US20120171502 A1 US 20120171502A1 US 201113188575 A US201113188575 A US 201113188575A US 2012171502 A1 US2012171502 A1 US 2012171502A1
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cerium
substrate
layer
chemical conversion
treatment solution
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US8784994B2 (en
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Hsin-Pei Chang
Wen-Rong Chen
Huann-Wu Chiang
Cheng-Shi Chen
Dun Mao
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Hongfujin Precision Industry Shenzhen Co Ltd
Hon Hai Precision Industry Co Ltd
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Hongfujin Precision Industry Shenzhen Co Ltd
Hon Hai Precision Industry Co Ltd
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    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23GCLEANING OR DE-GREASING OF METALLIC MATERIAL BY CHEMICAL METHODS OTHER THAN ELECTROLYSIS
    • C23G1/00Cleaning or pickling metallic material with solutions or molten salts
    • C23G1/02Cleaning or pickling metallic material with solutions or molten salts with acid solutions
    • C23G1/12Light metals
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/02Pretreatment of the material to be coated
    • C23C14/024Deposition of sublayers, e.g. to promote adhesion of the coating
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/0641Nitrides
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/0664Carbonitrides
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/0676Oxynitrides
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C22/00Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C22/05Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions
    • C23C22/06Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions using aqueous acidic solutions with pH less than 6
    • C23C22/48Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions using aqueous acidic solutions with pH less than 6 not containing phosphates, hexavalent chromium compounds, fluorides or complex fluorides, molybdates, tungstates, vanadates or oxalates
    • C23C22/57Treatment of magnesium or alloys based thereon
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C22/00Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C22/82After-treatment
    • C23C22/83Chemical after-treatment
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23FNON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
    • C23F1/00Etching metallic material by chemical means
    • C23F1/10Etching compositions
    • C23F1/14Aqueous compositions
    • C23F1/32Alkaline compositions
    • C23F1/40Alkaline compositions for etching other metallic material

Definitions

  • the disclosure generally relates to a process for surface treating magnesium alloy, and articles made of magnesium alloy treated by the process.
  • Magnesium alloys are widely used in manufacturing components (such as housings) of electronic devices and cars because of their properties such as light weight and quick heat dissipation.
  • magnesium alloys have a relatively low erosion resistance and abrasion resistance.
  • One method for enhancing the erosion resistance of magnesium alloy is to form ceramic coatings on its surface.
  • a lot of cast magnesium alloy has many pinholes on its surface. The ceramic coatings over these pinholes are usually thinner and weaker than other portions having no pinhole, rendering pitting corrosion more likely at these locations.
  • FIG. 1 is a cross-sectional view of an exemplary article treated in accordance with the present process.
  • FIG. 2 is a block diagram of a process for the surface treating of magnesium alloy according to an exemplary embodiment.
  • FIG. 3 is a schematic view of a vacuum sputtering machine for processing the exemplary article shown in FIG. 1 .
  • an exemplary process for the surface treatment of magnesium alloy may include steps S 1 to S 4 .
  • a substrate 11 is provided.
  • the substrate 11 is made of a magnesium alloy, such as Mg—Al alloy, or Mg—Al—Zn alloy.
  • step S 2 the substrate 11 is pretreated.
  • the pretreatment may include the following steps.
  • the substrate 11 is chemically degreased with an aqueous solution, to remove impurities such as grease or dirt from the substrate 11 .
  • the aqueous solution may contain about 25 g/L-30 g/L sodium carbonate (Na 2 CO 3 ), about 20 g/L-25 g/L trisodium phosphate dodecahydrate (Na 3 PO 4 .12H 2 O), and an emulsifier.
  • the emulsifier may be a trade name emulsifier OP-10 (a condensation product of alkylphenol and ethylene oxide) at a concentration of about 1 g/L-3 g/L.
  • the substrate 11 is immersed in the aqueous solution at a temperature of about 60° C.-80° C. for about 30 s-60 s. Then, the substrate 11 is rinsed for about 20 s-60 s.
  • the degreased substrate 11 is etched in an alkaline etchant, to create a smooth surface and further remove any impurities thereon.
  • the alkaline etchant is an aqueous solution containing about 40 g/L-70 g/L sodium hydroxide (NaOH), about 10 g/L-20 g/L Na 3 PO 4 .12H 2 O, about 25 g/L-30 g/L Na 2 CO 3 , and about 40 g/L-50 g/L sodium fluoride (NaF).
  • the substrate 11 is immersed in the alkaline etchant maintained at a temperature of about 40° C.-50° C. for about 3 s-5 s. During this process, burrs and other small sized protrusions are dissolved.
  • step S 3 when the pretreatment is finished, the substrate 11 undergoes a chemical conversion treatment, to form a cerium conversion film 13 .
  • the chemical conversion treatment applies a chemical conversion treatment solution containing cerium nitrate (Ce(NO 3 ) 3 ) and potassium permanganate (KMnO 4 ) as main film forming agents.
  • the chemical conversion treatment solution is an aqueous solution containing about 5 g/L-20 g/L Ce(NO 3 ) 3 , and about 2 g/L-10 g/L KMnO 4 .
  • the pH value of the chemical conversion treatment solution may be in a range between about 1 and 5.
  • the chemical conversion treatment may be carried out by immersing the substrate 11 in the chemical conversion treatment solution, which is maintained at about 20° C.-50° C., for about 15 min to 50 min.
  • the chemical conversion treatment solution is an aqueous solution containing about 11 g/L Ce(NO 3 ) 3 , and about 4 g/L KMnO 4 .
  • the pH value of the chemical conversion treatment solution is about 2.
  • the substrate 11 is immersed in the chemical conversion treatment solution maintained at about 35° C. for about 20 min. During the immersion, the chemical conversion treatment solution may be stirred.
  • a cerium conversion film 13 mainly comprising hydroxide and oxide of trivalent cerium, tetravalent cerium, and divalent manganese is formed on the substrate 11 .
  • a ceramic coating 15 is formed on the cerium conversion film 13 by physical vapor deposition, such as magnetron sputtering or arc ion plating.
  • the ceramic coating 15 may be single layer or multilayer refractory metal compound.
  • the refractory metal compound can be selected from one or more of the group consisting of nitride of titanium, aluminum, chromium, zirconium, or cobalt; carbonitride of titanium, aluminum, chromium, zirconium, or cobalt; and oxynitride of titanium, aluminum, chromium, zirconium, or cobalt.
  • the ceramic coating 15 includes a first layer 151 coated on the cerium conversion film 13 and a second layer 152 on the first layer 151 .
  • the first layer 151 is an aluminum-oxygen compound layer.
  • the second layer 152 is a chromium-oxygen-nitrogen compound layer.
  • the first layer 151 is directly formed on the cerium conversion film 13 by vacuum sputtering.
  • the substrate 11 is held on a rotating bracket 33 in a chamber 31 of a vacuum sputtering machine 30 as shown in FIG. 3 .
  • the chamber 31 is evacuated to maintain an internal pressure of about 6 ⁇ 10 ⁇ 3 Pa to 8 ⁇ 10 ⁇ 3 Pa and the inside of the chamber 31 is heated to a temperature of about 100° C. to about 150° C.
  • the speed of the rotating bracket 33 is about 0.5 revolutions per minute (rpm) to about 1.0 rpm.
  • Argon and oxygen are simultaneously fed into the chamber 31 , with the argon acting as a sputtering gas, and the oxygen acting as a reactive gas.
  • the flow rate of argon is about 150 standard-state cubic centimeters per minute (sccm) to about 300 sccm.
  • the flow rate of oxygen is about 50 sccm to 90 sccm.
  • a bias voltage of about ⁇ 100 volts (V) to about ⁇ 300 V is applied to the substrate 11 .
  • About 8 kW to about 10 kW of electric power is applied to aluminum targets 35 fixed in the chamber 31 , depositing the first layer 151 on the cerium conversion film 13 .
  • Depositing the first layer 151 may take about 30 min to about 60 min.
  • the power may be medium-frequency AC power.
  • the second layer 152 is directly formed on the first layer 151 also by vacuum sputtering. This step may be carried out in the vacuum sputtering machine 30 .
  • the aluminum targets 35 are switched off.
  • Argon, oxygen, and nitrogen are simultaneously fed into the chamber 31 .
  • the flow rate of oxygen is adjusted to about 40 sccm to about 100 sccm, and the flow rate of nitrogen is about 30 sccm to about 60 sccm.
  • About 8 kW to about 10 kW of electric power is applied to chromium targets 37 fixed in the chamber 31 , depositing the second layer 152 on the first layer 151 .
  • Depositing the second layer 152 may take about 30 min to about 120 min. Other parameters are the same as during deposition of the first layer 151 .
  • the cerium conversion film 13 has a good chemical stability and high compact density, with a good erosion resistance.
  • the cerium conversion film 13 provides a smooth surface on the substrate 11 , and by such means the ceramic coating 15 formed on the cerium conversion film 13 has a substantially even thickness, reducing the susceptibility to pit corrosion. Composed of refractory metal compounds and having a high abrasion resistance, the ceramic coating 13 protects the cerium conversion film 12 from mechanical abrasion.
  • FIG. 1 shows a cross-section of an exemplary article 10 made of magnesium alloy and processed by the surface treatment process as described above.
  • the article 10 may be a housing for an electronic device, such as a mobile phone.
  • the article 10 includes the substrate 11 made of magnesium alloy, the cerium conversion film 13 formed on the substrate 11 , and the ceramic coating 15 formed on the cerium conversion film 13 .
  • the cerium conversion film 13 is formed by a chemical conversion treatment using a chemical conversion treatment solution containing Ce(NO 3 ) 3 and KMnO 4 as main film forming agents, as described above.
  • the ceramic coating 15 may be a single layer or multilayer refractory metal compound.
  • the refractory metal compound can be selected from one or more of the group consisting of nitride of titanium, aluminum, chromium, zirconium, or cobalt; carbonitride of titanium, aluminum, chromium, zirconium, or cobalt; and oxynitride of titanium, aluminum, chromium, zirconium, or cobalt.
  • the ceramic coating 15 orderly includes a first layer 151 coated on the cerium conversion film 13 , and a second layer 152 on the first layer 151 .
  • the first layer 151 is an aluminum-oxygen compound layer.
  • the second layer 152 is a chromium-oxygen-nitrogen compound layer.
  • a neutral salt spray test was applied to the samples created by the present process.
  • the test conditions included 5% NaCl (similar to salt-fog chloride levels), and the test was an accelerated corrosion test for assessing coating performance. Erosion began to be observed after about 72 hours, indicating that the samples resulting from the present process have a good erosion resistance.

Abstract

A process for treating the surface of magnesium alloy comprises providing a substrate made of magnesium alloy. The substrate is then treated with a chemical conversion treatment solution containing cerium nitrate and potassium permanganate as main film forming agents, to form a cerium conversion film on the substrate. A ceramic coating comprising refractory metal compound is next formed on the cerium conversion film by physical vapor deposition.

Description

    CROSS-REFERENCE TO RELATED APPLICATIONS
  • This application is related to co-pending U.S. patent applications (Attorney Docket No. US35144, US36043, and US36044, each entitled “PROCESS FOR SURFACE TREATING MAGNESIUM ALLOY AND ARTICLE MADE WITH SAME”, each invented by Chang et al. These applications have the same assignee as the present application. The above-identified applications are incorporated herein by reference.
  • BACKGROUND
  • 1. Technical Field
  • The disclosure generally relates to a process for surface treating magnesium alloy, and articles made of magnesium alloy treated by the process.
  • 2. Description of Related Art
  • Magnesium alloys are widely used in manufacturing components (such as housings) of electronic devices and cars because of their properties such as light weight and quick heat dissipation. However, magnesium alloys have a relatively low erosion resistance and abrasion resistance. One method for enhancing the erosion resistance of magnesium alloy is to form ceramic coatings on its surface. However, a lot of cast magnesium alloy has many pinholes on its surface. The ceramic coatings over these pinholes are usually thinner and weaker than other portions having no pinhole, rendering pitting corrosion more likely at these locations.
  • Therefore, there is room for improvement within the art.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • Many aspects of the embodiments can be better understood with reference to the following drawings. The components in the drawings are not necessarily drawn to scale, the emphasis instead being placed upon clearly illustrating the principles of the exemplary process for the surface treating of magnesium alloy and articles made of magnesium alloy treated by the process. Moreover, in the drawings, like reference numerals designate corresponding parts throughout the several views. Wherever possible, the same reference numbers are used throughout the drawings to refer to the same or like elements of an embodiment.
  • FIG. 1 is a cross-sectional view of an exemplary article treated in accordance with the present process.
  • FIG. 2 is a block diagram of a process for the surface treating of magnesium alloy according to an exemplary embodiment.
  • FIG. 3 is a schematic view of a vacuum sputtering machine for processing the exemplary article shown in FIG. 1.
  • DETAILED DESCRIPTION
  • Referring to FIG. 2, an exemplary process for the surface treatment of magnesium alloy may include steps S1 to S4.
  • In step S1, referring to FIG. 1, a substrate 11 is provided. The substrate 11 is made of a magnesium alloy, such as Mg—Al alloy, or Mg—Al—Zn alloy.
  • In step S2, the substrate 11 is pretreated. The pretreatment may include the following steps.
  • Firstly, the substrate 11 is chemically degreased with an aqueous solution, to remove impurities such as grease or dirt from the substrate 11. The aqueous solution may contain about 25 g/L-30 g/L sodium carbonate (Na2CO3), about 20 g/L-25 g/L trisodium phosphate dodecahydrate (Na3PO4.12H2O), and an emulsifier. The emulsifier may be a trade name emulsifier OP-10 (a condensation product of alkylphenol and ethylene oxide) at a concentration of about 1 g/L-3 g/L. The substrate 11 is immersed in the aqueous solution at a temperature of about 60° C.-80° C. for about 30 s-60 s. Then, the substrate 11 is rinsed for about 20 s-60 s.
  • Then, the degreased substrate 11 is etched in an alkaline etchant, to create a smooth surface and further remove any impurities thereon. The alkaline etchant is an aqueous solution containing about 40 g/L-70 g/L sodium hydroxide (NaOH), about 10 g/L-20 g/L Na3PO4.12H2O, about 25 g/L-30 g/L Na2CO3, and about 40 g/L-50 g/L sodium fluoride (NaF). The substrate 11 is immersed in the alkaline etchant maintained at a temperature of about 40° C.-50° C. for about 3 s-5 s. During this process, burrs and other small sized protrusions are dissolved.
  • In step S3, when the pretreatment is finished, the substrate 11 undergoes a chemical conversion treatment, to form a cerium conversion film 13. The chemical conversion treatment applies a chemical conversion treatment solution containing cerium nitrate (Ce(NO3)3) and potassium permanganate (KMnO4) as main film forming agents. The chemical conversion treatment solution is an aqueous solution containing about 5 g/L-20 g/L Ce(NO3)3, and about 2 g/L-10 g/L KMnO4. The pH value of the chemical conversion treatment solution may be in a range between about 1 and 5. The chemical conversion treatment may be carried out by immersing the substrate 11 in the chemical conversion treatment solution, which is maintained at about 20° C.-50° C., for about 15 min to 50 min. In an exemplary embodiment, the chemical conversion treatment solution is an aqueous solution containing about 11 g/L Ce(NO3)3, and about 4 g/L KMnO4. The pH value of the chemical conversion treatment solution is about 2. The substrate 11 is immersed in the chemical conversion treatment solution maintained at about 35° C. for about 20 min. During the immersion, the chemical conversion treatment solution may be stirred. By this process, anions in the chemical conversion treatment agent react with metal atoms on a surface layer of the substrate 11, thus a cerium conversion film 13 mainly comprising hydroxide and oxide of trivalent cerium, tetravalent cerium, and divalent manganese is formed on the substrate 11.
  • In step S4, a ceramic coating 15 is formed on the cerium conversion film 13 by physical vapor deposition, such as magnetron sputtering or arc ion plating. The ceramic coating 15 may be single layer or multilayer refractory metal compound. The refractory metal compound can be selected from one or more of the group consisting of nitride of titanium, aluminum, chromium, zirconium, or cobalt; carbonitride of titanium, aluminum, chromium, zirconium, or cobalt; and oxynitride of titanium, aluminum, chromium, zirconium, or cobalt. In this exemplary embodiment, the ceramic coating 15 includes a first layer 151 coated on the cerium conversion film 13 and a second layer 152 on the first layer 151. The first layer 151 is an aluminum-oxygen compound layer. The second layer 152 is a chromium-oxygen-nitrogen compound layer. An exemplary process for forming the ceramic coating 15 may be performed by the following steps.
  • The first layer 151 is directly formed on the cerium conversion film 13 by vacuum sputtering. The substrate 11 is held on a rotating bracket 33 in a chamber 31 of a vacuum sputtering machine 30 as shown in FIG. 3. The chamber 31 is evacuated to maintain an internal pressure of about 6×10−3 Pa to 8×10−3 Pa and the inside of the chamber 31 is heated to a temperature of about 100° C. to about 150° C. The speed of the rotating bracket 33 is about 0.5 revolutions per minute (rpm) to about 1.0 rpm. Argon and oxygen are simultaneously fed into the chamber 31, with the argon acting as a sputtering gas, and the oxygen acting as a reactive gas. The flow rate of argon is about 150 standard-state cubic centimeters per minute (sccm) to about 300 sccm. The flow rate of oxygen is about 50 sccm to 90 sccm. A bias voltage of about −100 volts (V) to about −300 V is applied to the substrate 11. About 8 kW to about 10 kW of electric power is applied to aluminum targets 35 fixed in the chamber 31, depositing the first layer 151 on the cerium conversion film 13. Depositing the first layer 151 may take about 30 min to about 60 min. The power may be medium-frequency AC power.
  • Subsequently, the second layer 152 is directly formed on the first layer 151 also by vacuum sputtering. This step may be carried out in the vacuum sputtering machine 30. The aluminum targets 35 are switched off. Argon, oxygen, and nitrogen are simultaneously fed into the chamber 31. The flow rate of oxygen is adjusted to about 40 sccm to about 100 sccm, and the flow rate of nitrogen is about 30 sccm to about 60 sccm. About 8 kW to about 10 kW of electric power is applied to chromium targets 37 fixed in the chamber 31, depositing the second layer 152 on the first layer 151. Depositing the second layer 152 may take about 30 min to about 120 min. Other parameters are the same as during deposition of the first layer 151.
  • The cerium conversion film 13 has a good chemical stability and high compact density, with a good erosion resistance. In addition, the cerium conversion film 13 provides a smooth surface on the substrate 11, and by such means the ceramic coating 15 formed on the cerium conversion film 13 has a substantially even thickness, reducing the susceptibility to pit corrosion. Composed of refractory metal compounds and having a high abrasion resistance, the ceramic coating 13 protects the cerium conversion film 12 from mechanical abrasion.
  • FIG. 1 shows a cross-section of an exemplary article 10 made of magnesium alloy and processed by the surface treatment process as described above. The article 10 may be a housing for an electronic device, such as a mobile phone. The article 10 includes the substrate 11 made of magnesium alloy, the cerium conversion film 13 formed on the substrate 11, and the ceramic coating 15 formed on the cerium conversion film 13.
  • The cerium conversion film 13 is formed by a chemical conversion treatment using a chemical conversion treatment solution containing Ce(NO3)3 and KMnO4 as main film forming agents, as described above. The ceramic coating 15 may be a single layer or multilayer refractory metal compound. The refractory metal compound can be selected from one or more of the group consisting of nitride of titanium, aluminum, chromium, zirconium, or cobalt; carbonitride of titanium, aluminum, chromium, zirconium, or cobalt; and oxynitride of titanium, aluminum, chromium, zirconium, or cobalt. In this exemplary embodiment, the ceramic coating 15 orderly includes a first layer 151 coated on the cerium conversion film 13, and a second layer 152 on the first layer 151. The first layer 151 is an aluminum-oxygen compound layer. The second layer 152 is a chromium-oxygen-nitrogen compound layer.
  • A neutral salt spray test was applied to the samples created by the present process. The test conditions included 5% NaCl (similar to salt-fog chloride levels), and the test was an accelerated corrosion test for assessing coating performance. Erosion began to be observed after about 72 hours, indicating that the samples resulting from the present process have a good erosion resistance.
  • It is to be understood, however, that even through numerous characteristics and advantages of the exemplary disclosure have been set forth in the foregoing description, together with details of the system and functions of the disclosure, the disclosure is illustrative only, and changes may be made in detail, especially in matters of shape, size, and arrangement of parts within the principles of the disclosure to the full extent indicated by the broad general meaning of the terms in which the appended claims are expressed.

Claims (17)

1. A process for surface treating magnesium alloy, the process comprising the following steps of:
providing a substrate made of magnesium alloy;
forming a cerium conversion film on the substrate by treating the substrate with a chemical conversion treatment solution containing cerium nitrate and potassium permanganate as main film forming agents; and
forming a ceramic coating comprising refractory metal compound on the cerium conversion film by physical vapor deposition.
2. The process as claimed in claim 1, wherein the chemical conversion treatment solution is an aqueous solution containing about 5 g/L-20 g/L Ce(NO3)3, and about 2 g/L-10 g/L KMnO4; the pH value of the chemical conversion treatment solution is in a range between about 1 and 5.
3. The process as claimed in claim 2, wherein treating the substrate with the chemical conversion treatment solution is carried out by immersing the substrate in the chemical conversion treatment solution, which is maintained at a temperature of about 20° C.-50° C., for about 15 min to 50 min.
4. The process as claimed in claim 2, wherein the chemical conversion treatment solution is an aqueous solution containing about 11 g/L Ce(NO3)3, and about 4 g/L KMnO4; the pH value of the chemical conversion treatment solution is about 2.
5. The process as claimed in claim 4, wherein treating the substrate with the chemical conversion treatment solution is carried out by immersing the substrate in the chemical conversion treatment solution, which is maintained at a temperature of about 35° C., for about 20 min.
6. The process as claimed in claim 1, wherein the cerium conversion film mainly comprises hydroxide and oxide of trivalent cerium, tetravalent cerium, and divalent manganese.
7. The process as claimed in claimed 1, wherein the refractory metal compound is selected from one or more of the group consisting of nitride of titanium, aluminum, chromium, zirconium, or cobalt; carbonitride of titanium, aluminum, chromium, zirconium, or cobalt; and oxynitride of titanium, aluminum, chromium, zirconium, or cobalt.
8. The process as claimed in claimed 7, wherein the ceramic coating orderly includes a first layer coated on the cerium conversion film, and a second layer on the first layer, wherein the first layer is an aluminum-oxygen compound layer, the second layer is a chromium-oxygen-nitrogen compound layer.
9. The process as claimed in claim 1, wherein the physical vapor deposition uses a vacuum sputtering method or an arc ion plating method.
10. The process as claimed in claim 1, further comprising etching the substrate using an alkaline etchant containing about 40 g/L-70 g/L NaOH, about 10 g/L-20 g/L Na3PO4.12H2O, about 25 g/L-30 g/L Na2CO3, and about 40 g/L-50 g/L NaF, before treating the substrate with the chemical conversion treatment solution.
11. The process as claimed in claim 10, wherein the etching step is carried out by immersing the substrate in the alkaline etchant maintained at a temperature of about 40° C.-50° C. for about 3 s-5 s.
12. The process as claimed in claim 10, further comprising chemically degreasing the substrate, before the etching step.
13. An article, comprising:
a substrate made of magnesium alloy;
a cerium conversion film formed on the substrate, the cerium conversion film being formed by chemical conversion treatment with a chemical conversion treatment solution containing cerium nitrate and potassium permanganate as main film forming agents; and
a ceramic coating comprising refractory metal compound formed on the cerium conversion film by physical vapor deposition.
14. The article as claimed in claim 13, wherein the cerium conversion film is formed by immersing the substrate in the chemical conversion treatment solution maintained at about 25° C.-50° C., for about 15 min to 50 min; the chemical conversion treatment solution is an aqueous solution containing about 5 g/L-20 g/L Ce(NO3)3, and about 2 g/L-10 g/L KMnO4; the pH value of the chemical conversion treatment solution is in a range between about 1 and 5.
15. The article as claimed in claim 14, wherein the cerium conversion film mainly comprises hydroxide and oxide of trivalent cerium, tetravalent cerium, and divalent manganese.
16. The article as claimed in claim 13, wherein the refractory metal compound is selected from one or more of the group consisting of nitride of titanium, aluminum, chromium, zirconium, or cobalt; carbonitride of titanium, aluminum, chromium, zirconium, or cobalt; and oxynitride of titanium, aluminum, chromium, zirconium, or cobalt.
17. The article as claimed in claim 16, wherein ceramic coating orderly includes a first layer coated on the cerium conversion film and a second layer on the first layer, wherein the first layer is an aluminum-oxygen compound layer, the second layer is a chromium-oxygen-nitrogen compound layer.
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